Zobrazeno 1 - 10
of 44
pro vyhledávání: '"Manoranjan Sinha"'
Autor:
Gueraiche Djahid, Karpovich Elena, Pikulev Maxim, Kuznetsov Alexander, Sergey Popov, Manoranjan Sinha
Publikováno v:
Fluids, Vol 7, Iss 11, p 340 (2022)
This study aimed to explore the directional stability issues of a previously studied light box-wing aircraft model with a pusher propeller engine in the fuselage aft section. Earlier configurations have included the use of fuselage together with a li
Externí odkaz:
https://doaj.org/article/d1029273adde4da885582658b3a1aad3
Autor:
Saumitra Barman, Manoranjan Sinha
Publikováno v:
Journal of Guidance, Control, and Dynamics. 46:838-855
Attitude dynamics of a rigid satellite actuated using a double-gimbal variable-speed control moment gyro (DGVSCMG) with an unbalanced rotor is derived in the framework of geometric mechanics. The proposed formulation accounts for dynamics of the gimb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b739a5fd5ed1639720ae2294b7ed7e6
https://doi.org/10.2514/1.g006913
https://doi.org/10.2514/1.g006913
Autor:
Saumitra Barman, Manoranjan Sinha
Publikováno v:
Journal of Guidance, Control, and Dynamics. :1-17
A single-loop control architecture is proposed to achieve singularity-free attitude control of satellites actuated using a double-gimbal variable-speed control moment gyroscope (DGVSCMG). Satellite and DGVSCMG combined rotational dynamics is modeled
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b0ecba42f0df5f08578fc3eab20bd59
https://doi.org/10.2514/1.g007054
https://doi.org/10.2514/1.g007054
Autor:
Gargi Das, Manoranjan Sinha
Publikováno v:
Journal of Guidance, Control, and Dynamics. 46:325-342
A double-gimbal variable-speed control moment gyro (DGVSCMG) is considered for attitude control of a rigid satellite for track-to-track maneuver. Satellite attitude tracking control involves precision and time limit. In addition, satellite attitude c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eb2431b4df051065d7dd86da09b98f07
https://doi.org/10.2514/1.g006949
https://doi.org/10.2514/1.g006949
Publikováno v:
Advances in Military Technology. 15:163-178
Centre-of-gravity (c.g.) of combat aircraft suffers significant lateral deviation due to asymmetric release of stores, leading to a highly nonlinear and coupled dynamics. Additional nonlinearity and coupling result when the aircraft attempts some sup
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f3acdb447ceb02d86ea1071151f107b
https://doi.org/10.3849/aimt.01314
https://doi.org/10.3849/aimt.01314
Autor:
Saumitra Barman, Manoranjan Sinha
Publikováno v:
European Journal of Control. 70:100782
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6b301c85524403b4e1285be1a7b60653
https://doi.org/10.1016/j.ejcon.2023.100782
https://doi.org/10.1016/j.ejcon.2023.100782
Autor:
Manoranjan Sinha, Dipak Kumar Giri
Publikováno v:
Journal of Spacecraft and Rockets. 56:1636-1645
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29a7e8c07a88b6969a2dbb7dba5b32c7
https://doi.org/10.2514/1.a34475
https://doi.org/10.2514/1.a34475
Autor:
Manoranjan Sinha, Dipak Kumar Giri
Publikováno v:
Journal of Spacecraft and Rockets. 56:298-305
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8407fcae8c46415616ad1da28ff1681e
https://doi.org/10.2514/1.a34298
https://doi.org/10.2514/1.a34298
Publikováno v:
Aerospace Science and Technology. 121:107316
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79bf86a56c438d2f1427a648d271db4b
https://doi.org/10.1016/j.ast.2021.107316
https://doi.org/10.1016/j.ast.2021.107316
Publikováno v:
Acta Astronautica. 151:206-216
An adaptive fault-tolerant nonlinear control scheme is proposed for precise 3-axis attitude tracking of miniature spacecraft in the presence of control input saturation, model uncertainties, external disturbances, and reaction wheel faults. Two confi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f444dbb3358c59392445e6ff993e33e3
https://doi.org/10.1016/j.actaastro.2018.05.004
https://doi.org/10.1016/j.actaastro.2018.05.004